Thermal-IR Spectral Analysis of Jupiter's Trojan Asteroids
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Occultation Evidence for a Satellite of the Trojan Asteroid (911) Agamemnon Bradley Timerson1, John Brooks2, Steven Conard3, David W
Occultation Evidence for a Satellite of the Trojan Asteroid (911) Agamemnon Bradley Timerson1, John Brooks2, Steven Conard3, David W. Dunham4, David Herald5, Alin Tolea6, Franck Marchis7 1. International Occultation Timing Association (IOTA), 623 Bell Rd., Newark, NY, USA, [email protected] 2. IOTA, Stephens City, VA, USA, [email protected] 3. IOTA, Gamber, MD, USA, [email protected] 4. IOTA, KinetX, Inc., and Moscow Institute of Electronics and Mathematics of Higher School of Economics, per. Trekhsvyatitelskiy B., dom 3, 109028, Moscow, Russia, [email protected] 5. IOTA, Murrumbateman, NSW, Australia, [email protected] 6. IOTA, Forest Glen, MD, USA, [email protected] 7. Carl Sagan Center at the SETI Institute, 189 Bernardo Av, Mountain View CA 94043, USA, [email protected] Corresponding author Franck Marchis Carl Sagan Center at the SETI Institute 189 Bernardo Av Mountain View CA 94043 USA [email protected] 1 Keywords: Asteroids, Binary Asteroids, Trojan Asteroids, Occultation Abstract: On 2012 January 19, observers in the northeastern United States of America observed an occultation of 8.0-mag HIP 41337 star by the Jupiter-Trojan (911) Agamemnon, including one video recorded with a 36cm telescope that shows a deep brief secondary occultation that is likely due to a satellite, of about 5 km (most likely 3 to 10 km) across, at 278 km ±5 km (0.0931″) from the asteroid’s center as projected in the plane of the sky. A satellite this small and this close to the asteroid could not be resolved in the available VLT adaptive optics observations of Agamemnon recorded in 2003. -
Occultation Newsletter Volume 8, Number 4
Volume 12, Number 1 January 2005 $5.00 North Am./$6.25 Other International Occultation Timing Association, Inc. (IOTA) In this Issue Article Page The Largest Members Of Our Solar System – 2005 . 4 Resources Page What to Send to Whom . 3 Membership and Subscription Information . 3 IOTA Publications. 3 The Offices and Officers of IOTA . .11 IOTA European Section (IOTA/ES) . .11 IOTA on the World Wide Web. Back Cover ON THE COVER: Steve Preston posted a prediction for the occultation of a 10.8-magnitude star in Orion, about 3° from Betelgeuse, by the asteroid (238) Hypatia, which had an expected diameter of 148 km. The predicted path passed over the San Francisco Bay area, and that turned out to be quite accurate, with only a small shift towards the north, enough to leave Richard Nolthenius, observing visually from the coast northwest of Santa Cruz, to have a miss. But farther north, three other observers video recorded the occultation from their homes, and they were fortuitously located to define three well- spaced chords across the asteroid to accurately measure its shape and location relative to the star, as shown in the figure. The dashed lines show the axes of the fitted ellipse, produced by Dave Herald’s WinOccult program. This demonstrates the good results that can be obtained by a few dedicated observers with a relatively faint star; a bright star and/or many observers are not always necessary to obtain solid useful observations. – David Dunham Publication Date for this issue: July 2005 Please note: The date shown on the cover is for subscription purposes only and does not reflect the actual publication date. -
On the Accuracy of Restricted Three-Body Models for the Trojan Motion
DISCRETE AND CONTINUOUS Website: http://AIMsciences.org DYNAMICAL SYSTEMS Volume 11, Number 4, December 2004 pp. 843{854 ON THE ACCURACY OF RESTRICTED THREE-BODY MODELS FOR THE TROJAN MOTION Frederic Gabern1, Angel` Jorba1 and Philippe Robutel2 Departament de Matem`aticaAplicada i An`alisi Universitat de Barcelona Gran Via 585, 08007 Barcelona, Spain1 Astronomie et Syst`emesDynamiques IMCCE-Observatoire de Paris 77 Av. Denfert-Rochereau, 75014 Paris, France2 Abstract. In this note we compare the frequencies of the motion of the Trojan asteroids in the Restricted Three-Body Problem (RTBP), the Elliptic Restricted Three-Body Problem (ERTBP) and the Outer Solar System (OSS) model. The RTBP and ERTBP are well-known academic models for the motion of these asteroids, and the OSS is the standard model used for realistic simulations. Our results are based on a systematic frequency analysis of the motion of these asteroids. The main conclusion is that both the RTBP and ERTBP are not very accurate models for the long-term dynamics, although the level of accuracy strongly depends on the selected asteroid. 1. Introduction. The Restricted Three-Body Problem models the motion of a particle under the gravitational attraction of two point masses following a (Keple- rian) solution of the two-body problem (a general reference is [17]). The goal of this note is to discuss the degree of accuracy of such a model to study the real motion of an asteroid moving near the Lagrangian points of the Sun-Jupiter system. To this end, we have considered two restricted three-body problems, namely: i) the Circular RTBP, in which Sun and Jupiter describe a circular orbit around their centre of mass, and ii) the Elliptic RTBP, in which Sun and Jupiter move on an elliptic orbit. -
Comparison of the Physical Properties of the L4 and L5 Trojan Asteroids from ATLAS Data
Draft version January 13, 2021 Typeset using LATEX default style in AASTeX62 Comparison of the physical properties of the L4 and L5 Trojan asteroids from ATLAS data A. McNeill,1 N. Erasmus,2 D.E. Trilling,1, 2 J.P. Emery,1 J. L. Tonry,3 L. Denneau,3 H. Flewelling,3 A. Heinze,3 B. Stalder,4 and H.J. Weiland3 1Department of Astronomy and Planetary Science, Northern Arizona University, Flagstaff, AZ 86011, USA 2South African Astronomical Observatory, Cape Town, 7925, South Africa. 3Institute for Astronomy, University of Hawaii, Honolulu, HI 9682, USA. 4Vera C. Rubin Observatory Project Office, 950 N. Cherry Ave, Tucson, AZ, USA ABSTRACT Jupiter has nearly 8000 known co-orbital asteroids orbiting in the L4 and L5 Lagrange points called Jupiter Trojan asteroids. Aside from the greater number density of the L4 cloud the two clouds are in many ways considered to be identical. Using sparse photometric data taken by the Asteroid Terrestrial-impact Last Alert System (ATLAS) for 863 L4 Trojans and 380 L5 Trojans we derive the shape distribution for each of the clouds and find that, on average, the L4 asteroids are more elongated than the L5 asteroids. This shape difference is most likely due to the greater collision rate in the L4 cloud that results from its larger population. We additionally present the phase functions and c − o colours of 266 objects. Keywords: Jupiter trojans | multi-color photometry | sky surveys 1. INTRODUCTION Jupiter Trojans are minor planets that orbit 60 degrees ahead of (L4) and behind (L5) Jupiter in the 1:1 resonant Lagrange points. -
Structure and Composition of the Surfaces of Trojan Asteroids from Reflection and Emission Spectroscopy
Lunar and Planetary Science XXXVII (2006) 2075.pdf STRUCTURE AND COMPOSITION OF THE SURFACES OF TROJAN ASTEROIDS FROM REFLECTION AND EMISSION SPECTROSCOPY. Joshua. P. Emery,1 Dale. P. Cruikshank,2 and Jeffrey Van Cleve3 1NASA Ames / SETI Institute ([email protected]), 2NASA Ames Research Center ([email protected]), 3 Ball Aerospace ([email protected]). Introduction: The orbits of Trojan asteroids (~5.2 AU – beyond the Main Belt) place them in the transi- 1.0 tion region between the rocky inner and icy outer Solar 0.9 1172 Aneas System. Most Trojans were traditionally thought to 0.8 have originated in this region [3], although other loca- 1.0 tions of origin are possible [e.g., 4,5,6]. Possible con- 0.9 nections between Trojans and other groups of objects 911 Agamemnon 0.8 (Jupiter family comets, irregular satellites, Centaurs, Emissivity KBOs) are also important, but only poorly understood 1.0 [4,6,7,9]. The compositions of Trojans thereby hold 0.9 624 Hektor important clues concerning conditions in this critical 0.8 transition region, and the solar nebula as a whole. We discuss emission and reflection spectra of three Trojans 10 15 20 25 30 35 Wavelength (µm) (624 Hektor, 911 Agamemnon, and 1172 Aneas) and implications for surface structure and composition. Figure 2. Mid-IR emissivity spectra of Trojans. Vis-NIR Reflectance Spectroscopy: Reflectance studies of Trojans in the visible and NIR (0.8 – 4.0 Analysis: The Trojans have a similar spectral shape µm) reveal dark surfaces with mild to very red spectral to some carbonaceous meteorites and fine-grained sili- slopes, but no distinct absorption features (Fig. -
Astrocladistics of the Jovian Trojan Swarms
MNRAS 000,1–26 (2020) Preprint 23 March 2021 Compiled using MNRAS LATEX style file v3.0 Astrocladistics of the Jovian Trojan Swarms Timothy R. Holt,1,2¢ Jonathan Horner,1 David Nesvorný,2 Rachel King,1 Marcel Popescu,3 Brad D. Carter,1 and Christopher C. E. Tylor,1 1Centre for Astrophysics, University of Southern Queensland, Toowoomba, QLD, Australia 2Department of Space Studies, Southwest Research Institute, Boulder, CO. USA. 3Astronomical Institute of the Romanian Academy, Bucharest, Romania. Accepted XXX. Received YYY; in original form ZZZ ABSTRACT The Jovian Trojans are two swarms of small objects that share Jupiter’s orbit, clustered around the leading and trailing Lagrange points, L4 and L5. In this work, we investigate the Jovian Trojan population using the technique of astrocladistics, an adaptation of the ‘tree of life’ approach used in biology. We combine colour data from WISE, SDSS, Gaia DR2 and MOVIS surveys with knowledge of the physical and orbital characteristics of the Trojans, to generate a classification tree composed of clans with distinctive characteristics. We identify 48 clans, indicating groups of objects that possibly share a common origin. Amongst these are several that contain members of the known collisional families, though our work identifies subtleties in that classification that bear future investigation. Our clans are often broken into subclans, and most can be grouped into 10 superclans, reflecting the hierarchical nature of the population. Outcomes from this project include the identification of several high priority objects for additional observations and as well as providing context for the objects to be visited by the forthcoming Lucy mission. -
Trajectory Design of the Lucy Mission to Explore the Diversity of the Jupiter Trojans
70th International Astronautical Congress, Washington, DC. This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. IAC–2019–C1.2.11 Trajectory Design of the Lucy Mission to Explore the Diversity of the Jupiter Trojans Jacob A. Englander Aerospace Engineer, Navigation and Mission Design Branch, NASA Goddard Space Flight Center Kevin Berry Lucy Flight Dynamics Lead, Navigation and Mission Design Branch, NASA Goddard Space Flight Center Brian Sutter Totally Awesome Trajectory Genius, Lockheed Martin Space Systems, Littleton, CO Dale Stanbridge Lucy Navigation Team Chief, KinetX Aerospace, Simi Valley, CA Donald H. Ellison Aerospace Engineer, Navigation and Mission Design Branch, NASA Goddard Space Flight Center Ken Williams Flight Director, Space Navigation and Flight Dynamics Practice, KinetX Aerospace, Simi Valley, California James McAdams Aerospace Engineer, Space Navigation and Flight Dynamics Practice, KinetX Aerospace, Simi Valley, California Jeremy M. Knittel Aerospace Engineer, Space Navigation and Flight Dynamics Practice, KinetX Aerospace, Simi Valley, California Chelsea Welch Fantastically Awesome Deputy Trajectory Genius, Lockheed Martin Space Systems, Littleton, CO Hal Levison Principle Investigator, Lucy mission, Southwest Research Institute, Boulder, CO Lucy, NASA’s next Discovery-class mission, will explore the diversity of the Jupiter Trojan asteroids. The Jupiter Trojans are thought to be remnants of the early solar system that were scattered inward when the gas giants migrated to their current positions as described in the Nice model. There are two stable subpopulations, or “swarms,” captured at the Sun-Jupiter L4 and L5 regions. These objects are the most accessible samples of what the outer solar system may have originally looked like. -
The Minor Planet Bulletin
THE MINOR PLANET BULLETIN OF THE MINOR PLANETS SECTION OF THE BULLETIN ASSOCIATION OF LUNAR AND PLANETARY OBSERVERS VOLUME 38, NUMBER 2, A.D. 2011 APRIL-JUNE 71. LIGHTCURVES OF 10452 ZUEV, (14657) 1998 YU27, AND (15700) 1987 QD Gary A. Vander Haagen Stonegate Observatory, 825 Stonegate Road Ann Arbor, MI 48103 [email protected] (Received: 28 October) Lightcurve observations and analysis revealed the following periods and amplitudes for three asteroids: 10452 Zuev, 9.724 ± 0.002 h, 0.38 ± 0.03 mag; (14657) 1998 YU27, 15.43 ± 0.03 h, 0.21 ± 0.05 mag; and (15700) 1987 QD, 9.71 ± 0.02 h, 0.16 ± 0.05 mag. Photometric data of three asteroids were collected using a 0.43- meter PlaneWave f/6.8 corrected Dall-Kirkham astrograph, a SBIG ST-10XME camera, and V-filter at Stonegate Observatory. The camera was binned 2x2 with a resulting image scale of 0.95 arc- seconds per pixel. Image exposures were 120 seconds at –15C. Candidates for analysis were selected using the MPO2011 Asteroid Viewing Guide and all photometric data were obtained and analyzed using MPO Canopus (Bdw Publishing, 2010). Published asteroid lightcurve data were reviewed in the Asteroid Lightcurve Database (LCDB; Warner et al., 2009). The magnitudes in the plots (Y-axis) are not sky (catalog) values but differentials from the average sky magnitude of the set of comparisons. The value in the Y-axis label, “alpha”, is the solar phase angle at the time of the first set of observations. All data were corrected to this phase angle using G = 0.15, unless otherwise stated. -
Appendix 1 1311 Discoverers in Alphabetical Order
Appendix 1 1311 Discoverers in Alphabetical Order Abe, H. 28 (8) 1993-1999 Bernstein, G. 1 1998 Abe, M. 1 (1) 1994 Bettelheim, E. 1 (1) 2000 Abraham, M. 3 (3) 1999 Bickel, W. 443 1995-2010 Aikman, G. C. L. 4 1994-1998 Biggs, J. 1 2001 Akiyama, M. 16 (10) 1989-1999 Bigourdan, G. 1 1894 Albitskij, V. A. 10 1923-1925 Billings, G. W. 6 1999 Aldering, G. 4 1982 Binzel, R. P. 3 1987-1990 Alikoski, H. 13 1938-1953 Birkle, K. 8 (8) 1989-1993 Allen, E. J. 1 2004 Birtwhistle, P. 56 2003-2009 Allen, L. 2 2004 Blasco, M. 5 (1) 1996-2000 Alu, J. 24 (13) 1987-1993 Block, A. 1 2000 Amburgey, L. L. 2 1997-2000 Boattini, A. 237 (224) 1977-2006 Andrews, A. D. 1 1965 Boehnhardt, H. 1 (1) 1993 Antal, M. 17 1971-1988 Boeker, A. 1 (1) 2002 Antolini, P. 4 (3) 1994-1996 Boeuf, M. 12 1998-2000 Antonini, P. 35 1997-1999 Boffin, H. M. J. 10 (2) 1999-2001 Aoki, M. 2 1996-1997 Bohrmann, A. 9 1936-1938 Apitzsch, R. 43 2004-2009 Boles, T. 1 2002 Arai, M. 45 (45) 1988-1991 Bonomi, R. 1 (1) 1995 Araki, H. 2 (2) 1994 Borgman, D. 1 (1) 2004 Arend, S. 51 1929-1961 B¨orngen, F. 535 (231) 1961-1995 Armstrong, C. 1 (1) 1997 Borrelly, A. 19 1866-1894 Armstrong, M. 2 (1) 1997-1998 Bourban, G. 1 (1) 2005 Asami, A. 7 1997-1999 Bourgeois, P. 1 1929 Asher, D. -
Constraints on the Composition of Trojan Asteroid 624 Hektor Dale P
Constraints on the Composition of Trojan Asteroid 624 Hektor Dale P. Cruikshank 1'2 NASA Ames Research Center, MS 245-6, Moffett Field, California 94035-1000 E-mail: dcruikshank @ mail.arc.nasa.gov Cristina M. Dalle Ore SETI Institute and NASA Ames Research Center, MS 245-6, Moffett Field, California 94035-1000 Ted L. Roush NASA Ames Research Center, MS 245-3, Moffett Field, California 94035-1000 Thomas R. Geballe Gemini Observatory, 670 N. A'ohoku Place, Hilo, Hawaii 96720 Tobias C. Owen 1 Institute for Astronomy, 2680 Woodlawn Drive, Honolulu, Hawaii 96822 Catherine de Bergh 1 Observatoire de Paris, 4 Place Jules Jannsen, 92195 Meudon Cedex, France Michele D. Cash Stanford University, P.O. Box 16637, Stanford, California 94309 William K. Hartmann 2 Planetary Science Institute, 620 N. 6th Avenue, Tucson, Arizona 85715-8331 Submitted to Icarus December 12, 2000 Received Pages: 39 Figures: 7 Tables: 3 1. Guest observer, United Kingdom Infrared Telescope facility (UKIRT) 2. Guest observer, NASA Infrared Telescope Facility (IRTF) Proposed Running Head: Composition of Trojan Asteroid Hektor Address for Correspondence: Dale P. Cruikshank Mail Stop 245-6 NASA Ames Research Center Moffett Field, CA 94035-1000 dcruikshank @ mail.arc.n asa.gov Phone: 650-604-4244, Fax: 650-604-6779 Key Words: Asteroids, Composition Mineralogy Surfaces, Asteroids Spectroscopy ABSTRACT We presenta compositespectrumof Trojan asteroid624Hektor,0.3-3.6 p.m,which showsthatthereis no discernible3-p.mabsorptionband. Suchabandwould indicatethe presenceof OH or H20- bearing silicate minerals, or macromolecular carbon-rich organic material of the kind seen on the low-albedo hemisphere of Saturn's satellite Iapetus (Owen et al. -
(624) Hektor F
Asteroids, Comets, Meteors (2012) 6416.pdf PHYSICAL CHARACTERISTICS OF THE BINARY TROJAN ASTEROID (624) HEKTOR F. Marchis1,2, F. Vachier2, J. Durech3, J. Berthier2, M.H. Wong4, P. Kalas4, G. Duchene4,5,M. van Dam6, 1SETI Insti- tute ([email protected]) Carl Sagan Center, Mountain View CA USA, 2.IMCCE, Observatoire de Paris, France 3Astronomical Institute, Charles University in Prague, CzR 4Department of Asronomy, University of California, Berkeley USA, 5Observatoire de Grenoble, France 6. Flat Wavefronts, Christchurch, NZ Introduction: In July 2006, [1] announced the primary [10], we will derive the mass, hence the bulk discovery of a 15-km diameter satellite around the L4 density of Hektor. Jupiter Trojan asteroid (624) Hektor from direct obser- Preliminary Results: Genoid, genetic-based algo- vations using the W.M. Keck telescope. Over the past rithm [10], finds several prelimary solutions with ac- 6 years, our group has collected additional observa- ceptable fitting parameter 25<fp<50 milli-arcsec using tions to pinpoint the orbital parameters of Hektor’s a purely Keplerian orbit. All solutions have a period satellite, derive the mass of the system and thus infer P~2.98 days, a semi-major axis a between 1,100 and the average density of this large (Deq~225 km) Trojan 1,400 km and a significant eccentricity (e=0.13-0.20) asteroid. The density of the L5 double Trojan (617) which suggests an excited orbit (e.g. [4]). Using 3 Patroclus, estimated to be between 0.7-1.0 g/cm by [2] Deq~225 km, we derive a large density between 1.8 and (from IRAS) or 0.8-1.4 g/cm3 by [3], is the only den- 3.5 g/cm3. -
Occultation Newsletter Volume 8, Number 4
Volume 12, Number 1 January 2005 $5.00 North Am./$6.25 Other International Occultation Timing Association, Inc. (IOTA) In this Issue Article Page The Largest Members Of Our Solar System – 2005 . 4 Resources Page What to Send to Whom . 3 Membership and Subscription Information . 3 IOTA Publications. 3 The Offices and Officers of IOTA . .11 IOTA European Section (IOTA/ES) . .11 IOTA on the World Wide Web. Back Cover ON THE COVER: Steve Preston posted a prediction for the occultation of a 10.8-magnitude star in Orion, about 3° from Betelgeuse, by the asteroid (238) Hypatia, which had an expected diameter of 148 km. The predicted path passed over the San Francisco Bay area, and that turned out to be quite accurate, with only a small shift towards the north, enough to leave Richard Nolthenius, observing visually from the coast northwest of Santa Cruz, to have a miss. But farther north, three other observers video recorded the occultation from their homes, and they were fortuitously located to define three well- spaced chords across the asteroid to accurately measure its shape and location relative to the star, as shown in the figure. The dashed lines show the axes of the fitted ellipse, produced by Dave Herald’s WinOccult program. This demonstrates the good results that can be obtained by a few dedicated observers with a relatively faint star; a bright star and/or many observers are not always necessary to obtain solid useful observations. – David Dunham Publication Date for this issue: July 2005 Please note: The date shown on the cover is for subscription purposes only and does not reflect the actual publication date.